A propeller assembly (10) for aircrafts has a hub (12) having at least one receiver opening (16), a receiver (18) located within the receiver opening (16) and having a first collar (20) defining a blade opening (22), a blade (14) having a second collar (24) and a protrusion (26) with the second collar (24) abutting the first collar (20) and the protrusion (26) received within the blade opening (22), and a first retainer (32), and a second retainer (40).


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    Title :

    PROPELLER ASSEMBLY AND PROPELLER BLADE RETENTION ASSEMBLY FOR AIRCRAFTS


    Contributors:

    Publication date :

    2015-04-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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